科學(xué)研究與學(xué)術(shù)交流

首頁 >> 新聞中心 >> 科學(xué)研究與學(xué)術(shù)交流 >> 正文

Muzio Gola教授——描述透平葉片緣板阻尼器動力學(xué)行為的一種通用幾何理論

發(fā)布日期:2024-02-27    作者:     來源:     點擊:

科技部高端外國專家引進計劃

“航空發(fā)動機葉片振動不確定性分析理論與設(shè)計方法”

系列學(xué)術(shù)報告

報告題目:A general geometrical theory of turbine blade underplatform dampers 描述透平葉片緣板阻尼器動力學(xué)行為的一種通用幾何理論

報告人:Muzio Gola 教授

主持人:吳亞光 副教授,范雨 副教授

報告時間:2024年2月20日,上午11:00-12:00

報告地點:北航沙河校區(qū)F座3樓“數(shù)字發(fā)動機”多功能會議室

報告摘要

A general geometric theory of underplatform dampers as a function of blade neck deflection and the resulting platform kinematics is proposed. In-plane treatment is compatible with Mode 1 blade vibration, in which the rigid-body platform rotation associated with pure neck bending largely predominates over other rotations. The method applies when the amplitude of platform vibrational rotation reaches at least (or is greater than) the minimum value required to have, at both ends of the forward and reverse half-cycles, the onset of full slip in the last contact element still in stick.

The objective is to present a general geometric theory for damper kinematics and damper-platform forces, for both the In-Phase and Out-of-Phase blade vibrations. The concept of equivalent virtual parallel geometry is introduced, which transforms a case with nonnegligible inclination between adjacent blades into one, more tractable, valid for a very large (ideally infinite) number of blades.

The concept of a force Base-Cycle is introduced for the contact forces. Base Cycles uniquely characterize a damper shape so that, once produced for a convenient Reference Case, they can be scaled linearly without recalculation.

主講人簡介

Muzio Gola is Emeritus Professor in Department of Mechanical and Aerospace Engineering (DIMEAS) of Politecnico di Torino. He was the vice president of Polito. His main research interest focus on the mechanical aspects of aircraft turbine engines, such as: vibration and damping of turbine blades, underplatform damper design theory and experiments, contact mechanics in friction and wear at high temperature, thermal transients and fatigue in aircraft engine bladed disks. He has published more than 200 papers and undertaken project funds of more than 4 million euros.

快速鏈接

版權(quán)所有 ? 2021  北京航空航天大學(xué) 能源與動力工程學(xué)院
地址:北京市昌平區(qū)高教園南三街9號   電話010-61716819

射洪县| 黑龙江省| 浮山县| 长宁县| 怀柔区| 剑阁县| 资兴市| 明水县| 贵定县| 金溪县| 周口市| 尼勒克县| 阳江市| 乡城县| 昌宁县| 马关县| 隆回县| 余庆县| 龙州县| 崇阳县| 钦州市| 乐清市| 本溪市| 囊谦县| 宾川县| 六安市| 绥芬河市| 宝鸡市| 安龙县| 镇雄县| 射阳县| 城步| 长兴县| 望谟县| 鄂尔多斯市| 扎鲁特旗| 斗六市| 雷山县| 青龙| 牟定县| 海林市|